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PUMA SA - 330J

MANUFACTURE : AEROSPATIALE 1974



POWER PLANT

Power Plant :2 (two) Turmo IV.C Turbomeca 1558 Hp Each
Take Off Power :1494 SHP
Max. Contingengy Power :1262 SHP

SPECIFICATIONS

Seating Capacity :3 Cockpit + 17 Seat (airline), 18 Seat (troop)
Litter Capacity :6 Each
Avarage Cruise Speed :120 Kts
Speed with Slung Load :40 -100 Kts
Max. Speed (VNE) :167 Kts
Fuel Consumption :660 Ltr/hr
Fuel Capacity :Internal Tank : 1550 Ltr
  :External Tank : 700 Ltr
  :Ferry Tank (1) : 475 Ltr
Max. Range (15'''''''' Reserve) :379 Nm / 703 Km
Ceiling (T/O & Landing) :13000 ft
Ceiling (Inflight) :16500 ft
Max. Rate of Climb :1200 ft/min

DIMENSION

Rotor Blades :4 Fully Artriculated
Fuselage Length :14.82 M
Overall Length :18.2 M
Fuselage Width :3.0 M
Overall Height :5.14 M
Main Rotor Diameter :15.09 M
Tail Rotor Clearance :1.83 M
Cabin Doors Dimension :1.35 M x 1.35 M

LOADING INFORMATION

Max. Gross Weight :7400 Kg / 16300 Lb
Empty Weight - Std :4240 Kg / 9346 Lb
Usefuel Load - Int :3160 Kg / 6964 Lb
Usefuel Load - Ext :3260 Kg / 7185 Lb

HELIPAD SIZE

Size :20 x 20 M (Fato : 27.3 x 27.3 M )
Minimum Strenght :11.100 K